Scalable, electro-optically induced force system and method

ABSTRACT

A technique is disclosed for electro-optically inducing a force to fabricated samples and/or devices with laser light. The technique uses the interaction of the oscillating electric field of the laser beam in opposition with the electric field produced by an appropriate electric charge carrier to achieve a net repulsive (or attractive) force on the component holding the electric charge. In one embodiment, force is achieved when the field near the charge carrier is modulated at a subharmonic of the electric field oscillation frequency of the laser and the relative phases of the light field and electric charge carrier field are controlled to provide optimal repulsion/attraction. The effect is scalable by applying the technique to an array of charge carrier fields sequentially as well as using higher power lasers and higher carrier field voltages.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation-in-part of, and claims the benefit under 35 U.S.C. § 120 from, nonprovisional U.S. patent application Ser. No. 15/406,737, entitled “Scalable, electro-optically induced force system and method”, filed Jan. 15, 2017, now U.S. Pat. No. 9,984,782. The subject matter of each of the foregoing documents is expressly incorporated herein by reference.

TECHNICAL FIELD

The present invention relates generally to techniques for applying a force or inducing a change in momentum to objects using interacting electromagnetic fields and, particularly, to techniques for applying a force or inducing a change in momentum to objects using a laser beam as one of the sources of the electromagnetic fields.

BACKGROUND

The manipulation of samples or devices through the use of electromagnetic (EM) radiation has a number of advantages over mechanical or “tactile” manipulation.

Typically, EM manipulation is less mechanically destructive and can be accomplished through mechanical barriers where other more traditional means are not effective. EM manipulation has become more prevalent as technology has advanced and is now accomplished through both constant field applications (as in the case of superconductor facilitated magnetically induced levitation) and oscillating field applications (e.g. laser assisted cooling and trapping).

The manipulation of mass through the use of laser light has found many applications as laser technology has evolved. Not simply laser photolysis or spectroscopy, but coherent control of chemical reactions is becoming possible (see P. Brumer and M. Shapiro, Sci. Am., pg. 56, March 1995). Laser atom or molecule trapping has seen a great deal of activity (see S. Chu, Science, pg. 861, 23 Aug. 1991; C. N. Cohen-Tannoudji and W. D. Phillips, Phys. Today, pg. 33, October 1990) and has lead to the observation of Bose-Einstein condensation and the improvement of atomic clocks. Control of larger mass samples with laser energy has also been demonstrated. “Optical tweezers” have been used to stretch single strands of DNA and manipulate chromosomes inside cell nuclei and move entire cellular organelles without destroying the cell wall (see S. Chu, Sci. Am., pg. 71, February 1992). Standing wave laser radiation has also been used to deflect atomic beams in flight (see P. E. Moskowitz, P. L. Gould, and D. E. Pritchard, J. Opt. Soc. Am. B., 2, 11, 1784, 1985).

All of these techniques allow for control of small samples with laser light, but none of these is practically applicable to larger samples or efficiently uses the laser light to accomplish the manipulation. One of the difficulties is that many of the current techniques operate by inducing an electric charge polarization in the sample. The force which can be induced by the laser beam is directly related to the degree to which a sample can be polarized before it is damaged. The laser peak intensity must be controlled or the sample can be overheated, ionized or destroyed. This limits the achievable manipulation force. Also, these techniques commonly require the laser to be focused on the target sample, limiting the length of interaction and thus the efficiency with which the laser energy is coupled into translation. Other techniques rely on the transfer of photon momentum in the optical scattering process, but this is extremely inefficient as photons at commonly accessible wavelengths have very little mass.

Therefore, it is the object of the present invention to provide a system that 1) employs laser light to apply a force to objects that 2) is scalable, that 3) maximizes the efficiency with which the laser light is utilized for said force, that 4) the intensity of laser light employed by the system should not be limited by the risk of damage to the object upon which the force is induced.

SUMMARY OF THE INVENTION

The essence of electro-optically induced force and/or momentum is to mimic the repulsion manifested when two like charged wires come into proximity with one another. Wires carrying like charges repel one another due to the mutual opposition of the electric fields generated by the charges on the wires. An electro-optically induced force is realized when one of the wires is replaced with a substitute that maintains an electric field in opposition to the field generated by the first wire (e.g. a photon or radiation field). The principles employed by the present invention to electro-optically induce a force to manipulate objects are now described.

FIG. 1 shows a schematic of 1) the electric field around an electrically charged wire parallel to the Z-axis (i.e. perpendicular to the page of the schematic) (100), 2) the projection of said electric field on the Y-axis (vertical in the plane of the page), said projection is described by a sine function (102), 3) the electric field of a laser beam propagating in space perpendicular to the wire, 1) above (104), 4) the electric field of a laser beam retro reflected by a mirror with a surface perpendicular to the laser beam path (106).

FIG. 2 shows a schematic of the field interaction, in space at a given instant, between the electric field from a charged wire (200) and the electric field of a laser beam travelling proximate and perpendicular to the charged wire (202) (i.e. for those fields illustrated in FIG. 1). It should be noted that, in the case of a freely propagating laser, a continuous sine wave, and the Y-axis component of the electric field shown, a second sine wave, the net field interaction will always be zero, a function of the orthogonality of sine functions. But, in the case of a retro reflected laser beam, by positioning the retro reflecting mirror judiciously, the spatial relationship between the standing electric field of the wire (200) and the electric field of the laser (202) and can be chosen so the net field interaction between the electric field of the laser and the electric field near the wire, at the given moment illustrated, is non-zero. The net field interaction (204) is shown schematically in FIG. 2.

It should be noted that the spatial relationship between the electric field of the laser and the standing electric field near the wire can be altered, and a non-zero net field interaction achieved, using transmissive optics as well. A schematic is shown in FIG. 3. In this case, the change in refractive index, n, between the original propagation medium (e.g. air, for which n˜1) and the medium of the optic (e.g. glass, for which n˜1.5) gives rise to a phase change between the electric field near the wire along the propagation direction of the laser (300) and the electric field of the laser (302). This changes the integral of the interaction between the two electric fields (304) to a, potentially, non-zero value.

A final case is shown schematically in FIG. 4. The spatial relationship between the electric field near the wire (400) and the electric field of the laser (402) is altered by directing the laser through an aperture of an electrically conductive material. In such a case the conductive material screens the electric field near the wire (400) from interaction with the electric field of the laser (402) internal to the conductive material. This changes the integral of the interaction between the two electric fields (404) to a, potentially, non-zero value.

The above describes methods for achieving a non-zero net field interaction at a given moment in time, meaning a given phase of the laser light, but the electric field of a laser oscillates at frequency given by f=c/λ, where c is the speed of light and λ is the wavelength of the laser. This frequency is typically hundreds of terahertz, much faster than practical electronic signals can be generated, and so any momentary interaction between the laser and the standing electric field of the wire will quickly integrate to zero. In order to sustain and extend a net field interaction over time, it is necessary to vary the electric field near the wire.

FIG. 5 shows a schematic of the interactions, in time, between the electric field near a wire driven by a square waveform (500) and the electric field of a laser beam traveling proximate and perpendicular to the wire (502). The accumulated field interaction (504) over one period of the waveform driving the charge on the wire is given by F=∫ sin(ω₁(t))*f _(sg)(t,θ _(pm))∂t  eq. 1

and is shown schematically in FIG. 5. Where, ω₁ is the frequency of the laser beam, f_(sg) is the time-variant electric field near the wire, and θ_(pm) is the value of the time-variant optical phase modulation induced to the electric field near the wire.

It should be noted that, 1) depending on the relative phase of the given electric fields, the above integral (eq. 1) can be either positive or negative, corresponding to the case of generating a repulsive or attractive force, respectively and 2) although the waveform shown in FIG. 5 is a square wave, that need not be the case. Since the signal driving the electric field on the wire cantilever is electronically generated, f_(sg) can be configured as any function that is determined to facilitate the desired effect. Note is given to the case of a phase modulated sine wave.

Consider a specific case: a signal generator operating at 5.64 GHz and common laser wavelength, 532 nm or ˜5.64×10¹⁴ Hz. In this case, the laser is operating at a frequency that is one hundred thousand times faster than the signal generator. In this example, the electric field of the laser and the electric field induced near the wire may only be in opposition, in time, space, and intensity, a fraction measured in parts per million (ppm) depending on the specific wave shape and/or modulation induced to the electric field near the wire. But, as described below, a field carrier array may be constructed with very high density, with feature spacing in the sub-micron range. In such a case, one could achieve one million, or more, field interaction locations per meter, and so, even if the electric field of the laser and the electric field near the charge carrier are in opposition a small fraction of the time per oscillation at each location, integrating one million locations over the length of a one meter array, comprised of one million elements, can afford substantial accumulated force between the electric field of the laser and the electric field(s) near the array.

The teachings of the present invention are operable in systems where the electric fields are neither free-space nor produced by a laser. The present invention is generally directed to any electro-optical system including a charge carrier configured to carry a charge distribution that gives rise to a first electromagnetic field, and a radiation source configured to generate a second electromagnetic field that interacts with the first electromagnetic field so as to produce a net force on the charge carrier.

BRIEF DESCRIPTION OF THE FIGURES

Additional objects and features of the invention will be more readily apparent from the following detailed description and appended claims when taken in conjunction with the drawings, in which:

FIG. 1 is a schematic diagram illustrating the electric fields employed in the present invention.

FIG. 2 is a schematic diagram illustrating phase relationship between the electric fields employed in the present invention, retro-reflecting case.

FIG. 3 is a schematic diagram illustrating phase relationship between the electric fields employed in the present invention, transmissive optic case.

FIG. 4 is a schematic diagram illustrating phase relationship between the electric fields employed in the present invention, conductive screening case.

FIG. 5 is a schematic diagram illustrating the variations, in time, between the electric field of the laser and the electric field near the charge carrier, as well as the accumulated field product integral, representing the accumulated force on the carrier.

FIG. 6 is a schematic of a circuit that is configured to process a commercially available square wave into a signal sufficient to induce a measureable force between a continuous wave single frequency laser and a conductive wire cantilever.

FIG. 7 is a schematic diagram illustrating a first preferred embodiment of the present invention employing a continuous wave single frequency laser and a single field carrier.

FIG. 8 is a schematic diagram illustrating a preferred embodiment of the present invention employing a continuous wave single frequency laser and a field carrier array.

FIG. 9 is a schematic diagram illustrating the relationship between the electric fields employed in the present invention, free space case.

FIG. 10 is a schematic diagram illustrating a preferred embodiment of the present invention employing a continuous wave single frequency laser and a field carrier array, free space case.

FIG. 11 is a schematic of a circuit that is configured to process a commercially available sinusoidal signal into a signal sufficient to induce a measureable force between a continuous wave single frequency laser and a conductive wire cantilever: combiner case.

DETAILED DESCRIPTION

The present invention allows for the application of laser light to achieve a scalable electromagnetically induced force to samples of greater mass than previous techniques and for more efficient use of the applied laser light. The sample upon which the force is realized must be of specific construction to support an electric charge distribution and variation to achieve a net repulsion or attraction with the laser light. Using this approach the laser need not be focused on the sample nor induce an electric charge polarization on the sample. This allows the force to be integrated over a longer distance, greatly improving the efficiency with which the laser energy is used and increasing the mass amenable to manipulation by the techniques of the present invention.

Several recent advancements have driven this invention. First, the laser power available from smaller, less expensive devices is increasing continually. Laser devices are now being constructed that produce watts of laser energy from laser heads that are millimeters or even micrometers in size.

As for the magnitude of the accumulated force, let us consider the example of a 10 W laser. Currently such lasers can be fabricated at relatively low cost, and weigh on the order of grams. Ten Watts (10 N*m/s) of optical power, if converted entirely to work (N*m) could lift 1 kg of mass 1 meter per second against earth's gravity (9.8 m/s^2). An array of one thousand 10 W lasers, or the case of a single 10 kW laser, could potentially lift tons.

It is the object of this invention to be scalable and to enable such applications.

Second, laser energy efficiency is improving as technology advances. As an example, 35-60% of the energy spent to drive some laser diodes is converted directly to laser light energy.

Third, circuit features as smaller than 0.25 micrometers can now be fabricated and this technology continues to advance to fabricate features of even smaller size. This feature size is less than half the wavelength of light produced by many high power laser packages. The provides an excellent opportunity to construct a periodic charge distribution giving rise to a periodic electric field that can directly counter the periodic electric field of a laser beam. This is an ideal arrangement for electromagnetic repulsion/attraction (i.e., electro-optically induced force).

Single Frequency Laser Source Embodiments

Signal Generator System

FIG. 6 shows schematic of a circuit used to process a commercially available square wave into a signal sufficient to induce a measureable force between a continuous wave single frequency laser and a conductive wire cantilever. A square wave signal generator (600) is set to generate a drive signal at a subharmonic of the laser frequency (e.g. one hundred thousandth of the laser frequency). The output of the signal generator is directed through an adjustable delay line (602). It is advantageous to drive the signal at higher voltage since the field interactions sought scale with the field intensity and thus voltage applied. The signal can be amplified using a broadband amplifier (604) to increase the net force induced.

Commercially available signal sources (e.g. square wave clock generators) may have signal jitter in the 100 to 300 femtosecond range, but the laser electric field oscillation for commercially available single frequency lasers (e.g. a 532 nm laser) is approximately 2 femtoseconds. In such a case, the jitter of the square wave will preclude any efficient induction of force on the wire cantilever as it will tend to average out any net repulsion/attraction. It is necessary to improve the square wave signal jitter to provide for stable and efficient field interactions. To accomplish this, the processed square wave signal, described above, is directed into the forward port of a broadband directional coupler (606). The output of the directional coupler is sent to a third adjustable delay line (608) and back to the input port of the broadband coupler (606), creating a loop. The delay line (608) is adjusted to phase lock the resultant signal loop. In effect the delay line (608) is adjusted to ensure that the signal loop is an integer multiple of the square wave length. In such an arrangement, the jitter of the input signal is reduced by the square root of the number of round trips the signal makes in the loop. In the case of a 40 db power coupler, the jitter is improved by a factor of 10.

To improve the signal jitter further, the signal from the reference port of the broadband coupler (606) is directed to the forward port a second broadband coupler (610). The output of the second broadband coupler (610) is directed through a fourth delay line (612) and back to the input port of the second broadband directional coupler (610). The delay line (612) is adjusted to phase lock the second resultant signal loop. In effect the delay line (612) is adjusted to ensure that the second signal loop is also an integer multiple of the square wave length. Again, the jitter of the input signal is reduced by the square root of the number of round trips the signal makes in the second loop. In the case of a 40 db power coupler, the jitter is improved by a further factor of 10.

In the above description, two successive directional coupler stages should be sufficient to reduce the (e.g. 200 fs) jitter of the square wave clock generator source to a value comparable to the oscillation frequency of the single frequency laser source (approximately 2 fs), but successive stages of broadband couplers and paired delay lines can be employed to reduce the jitter to desired levels.

In this embodiment, the wire cantilever configured to achieve a repulsion with the single frequency laser, below, is within the second coupler (610)/delay line (612) loop described above. The interaction site (614) is shown schematically in FIG. 6. The signal from the reference port of the second directional coupler (610) is directed to a monitor oscilloscope (616).

FIG. 7, shows a schematic of a preferred embodiment. A continuous wave (CW) single frequency laser (700) produces a beam (702) that is directed to a retro-reflecting mirror (704) to provide the optical electromagnetic field which will induce a force at the wire cantilever site (614) described above and shown schematically in FIG. 6. The square wave clock generator (706), signal processing circuit (708), and monitor oscilloscope (710) are the same as those described in FIG. 6, (600), (602-612), and (616), respectively. The wire cantilever (712) consists of a length from the second directional coupler (610)/delay line (612), above, configured to be in close proximity (e.g. less than 1 mm) to the laser beam (702) and retro-reflecting mirror (704). The system is configured such that the linear polarization of the laser beam (702) is perpendicular to the wire cantilever (712).

Interferometric Force Detection System

A fiber optic force detection system similar to that used in atomic force microscope studies (D. Rugar, H. J. Mamin, and P. Guethner, Appl. Phys. Lett. 55, 25, (1989) 2588) is employed here to measure force induced between a wire cantilever loop (712) and a laser beam (702).

The output of a single-mode fiber-coupled probe laser (714) is directed into a single mode 2×2 fiber coupler (716). One optically cleaved end of the output fiber (718) of the fiber coupler (716) is positioned in close proximity (e.g. single microns) and perpendicular to the wire cantilever (712). A piezo electric actuator, PZT (720) is attached to the optical fiber (718) and driven by a signal generator (722). The PZT (720) drives the motion of the optical fiber (718) perpendicular to the wire cantilever (712).

The single frequency laser light exiting the output of the fiber coupler (718) is made incident upon the wire cantilever (712). A portion of the light exiting the optical fiber (718) and incident on the wire cantilever (712) is reflected back into the optical fiber (718) and co-propagates with the light reflected from the internal surface of the optically cleaved fiber (718).

The return signal, the optical interferometric signal between the counter propagating reflection of the optically cleaved end of the optical fiber (718) and the reflective surface of the wire cantilever (712), travels back through the optical fiber (718), back through the fiber coupler (716), and is directed into a detector photodiode (724). The output of the detector photodiode (724) is measured using a lock-in amplifier (726), using the reference signal from the signal generator (722) driving the PZT (720). The signal from the lock-in amplifier is observed on a monitor oscilloscope (728). A monitor photodiode (730) can be employed to measure the second output of the fiber coupler (716) to ensure system stability.

The constructive and destructive interference between the light reflected from the internal surface of the optically cleaved fiber (718) and the light reflected from the wire cantilever (712), driven and detected at the frequency of the lock-in amplifier (726), allows for a very sensitive detection of movement of the wire cantilever (712) (e.g. nanometers). When the wire cantilever (712) is chosen with a small force constant, this allows for very sensitive force detection (e.g. nanoNewtons).

Laser/Carrier Field Interaction

The choice of frequency of the square wave generator (706) is critical for manifestation of the desired effect. FIG. 5 shows a condition where the laser frequency (502) is an odd multiple of the cantilever driver frequency (500). In such a case, the positive, rising, half cycle of the square wave is integral over an extra (e.g. positive) half cycle of the laser oscillation and the negative, falling, half cycle of the square wave is integral over a complimentary (e.g. negative) half cycle of the laser oscillation. This frequency, and phase, relationship gives rise to cumulative, non-zero, field interaction (504) between the electric field of the laser (502) and the electric field near the wire cantilever (500) over time.

It has been noted, above, that depending on the relative phase of the given electric fields, the above integral (eq. 1) can be either positive or negative, corresponding to the case of generating a repulsive or attractive force, respectively, on the wire cantilever. In the present case, the relative phase between the oscillating electric field of the laser (700) and the oscillating electric field of the wire cantilever (712) can be easily achieved by adjusting the delay line of the signal processing circuit (602).

Carrier Array

FIG. 8 shows a schematic where a set of field carriers (e.g. a set of wire cantilevers, or alternatively a series of traces on a printed circuit board) (832) is arrayed perpendicular to and along a laser's (800) propagation path (802) and an equivalent set of transmissive optics (804) is paired with each field carrier to facilitate the process, as shown schematically in FIG. 3. The field carriers shown (834) share a common platform, so a single interferometric detection measurement (814-830), as shown in FIG. 7, is sufficient to measure the cumulative force on the ensemble of field carriers.

As the circuit path for each carrier is unique, each field carrier signal wave must have separate phase control to facilitate the desired effect. The phases are adjusted to maximize the force detected via the interferometric detector signal described above.

While the preferred embodiments, above, employ a single frequency laser, the techniques of the present invention are applicable to multi-mode lasers.

Multi-Mode Laser Embodiment

Typically, lasers that provide high output power operate in several longitudinal modes of the laser resonator cavity. The wavelengths of the cavity modes of any laser are given by the expression: n I=2L, where, n is an integer, I is the wavelength of the laser light, and L is the length of the laser resonator cavity. As a result, when a multi-mode laser is used several different wavelengths of laser light are produced simultaneously.

Therefore, the present invention also includes an embodiment that uses the laser light from multi-mode lasers by providing a path to match each of the laser's active laser cavity modes.

Free Space Laser Propagation Embodiment

It should be noted that the electric field near a set of charge carriers can be configured such that a non-zero net interaction with the electric field of the laser can be achieved, in the case where the laser is directed to travel proximate and perpendicular to the charge carriers in free space, with no optics in the laser beam path. A schematic is shown in FIG. 9. In this case, the charges on a set of separate carriers (e.g. a set of parallel traces on a PCB) are configured to achieve a non-sinusoidal electric field variation in the direction of laser travel (900). The electric field of the laser beam (902) is shown schematically over the same distance. In such a case, the space integral (904) of the electric field near the charge carrier array (900) and the electric field of the laser (902) can be a non-zero value.

FIG. 10 shows a schematic where a set of field carriers (e.g. a set of wire cantilevers, or alternatively a series of traces on a printed circuit board) (1032) is arrayed perpendicular to and along a laser's (1000) propagation path (1004). The field carriers shown share a common platform (1034), so a single interferometric detection measurement (1014-1030) is sufficient to measure the cumulative force on the ensemble of field carriers.

As the circuit path for each carrier (1032) is unique, each field carrier signal wave must have separate phase control to facilitate the desired effect. The phases are adjusted to maximize the force detected via the interferometric detector signal described above.

Jitter Reduction Circuit with Combiner Embodiment

FIG. 11 shows a schematic of an alternate embodiment of a circuit to reduce jitter in an electronic signal, the first embodiment having been presented in FIG. 6. In FIG. 11, a sinusoidal signal generator (e.g. 1 GHz, 300 fs jitter) (1100) is directed into a first input port of a first signal combiner (1102). The first signal combiner (1102) provides an isolation (e.g. 40 db) between the two input ports of the combiner (1102). The output of the first combiner (1102) is directed into the first input port of a, similar, second combiner (1104). The output of the second combiner (1104) is directed to the input of a first adjustable delay line (1106) and the output of the first delay line (1106) is directed into the second input port of the first combiner (1102), thereby creating a feedback loop that propagates through the first delay line (1106). When the delay line (1106) is adjusted such that the length of one round trip through the circuit (1102, 1104, and 1106) is an integral multiple of the wavelength of the signal from the signal generator (1100), the feedback loop serves to reduce both the jitter and amplitude noise of the input signal by the square root of the number of round trips through the circuit, determined by the isolation values of the combiners (1102 and 1104). As an example, if the combiners serve to transmit ninety nine percent of the signal from the first combiner input port to the combiner output port and one percent of the signal exits through the second input port of the combiner, a result of imperfect isolation, the number of round trips through the feedback loop would be approximately ninety eight. In such a case the noise in the above circuit would be reduced by the square root of approximately ninety eight, or nearly ten-fold.

In FIG. 11, a second combiner set is shown (1108 and 1110). The purpose of the second combiner set (1108 and 1110) is to reduce the signal noise further. The signal from the second input of the second combiner (1104), the leakage from the second combiner, is directed to the first input port of a third signal combiner (1108). The output of the third combiner (1108) is directed to the first input port of a fourth combiner (1110) and the output of the fourth combiner is directed to the input of a second adjustable delay line (1112). The output of the second delay line (1112) is directed to the second input of the third signal combiner (1108), thereby creating a second feedback loop. The length of the second feedback loop is adjusted to be an integral multiple of the wavelength of the signal from the signal generator (1100). Thus the second set of combiners (1108 and 1110) and the second delay line (1112) serve to further reduce the signal noise from the output of the second signal combiner (1104) (e.g. by a further factor of 10)

The signal, leakage, from the second input port of the fourth signal combiner (1110) is directed to a commercial circuit (1114) that converts a sinusoidal signal to a square wave signal, thus providing the signal upon the charge carriers in FIGS. 7, 8 and 10 (712, 812/832, and 1012/1032, respectively) sufficient to induce a measurable force between a continuous wave single frequency laser and a conductive charge carrier or series of charge carriers.

While the present invention has been described with reference to a few specific embodiments, the description is illustrative of the invention and is not to be construed as limiting the invention. Various modifications may occur to those skilled in the art without departing from the true spirit and scope of the invention as defined by the appended claims. 

What is claimed is:
 1. A system comprising: a signal generator that generates a first signal having a first jitter characteristic of a first value; a signal processing circuit that has a first input, a second input, and an output, wherein the first input is coupled to receive the signal generated by the signal generator, wherein the signal processing circuit generates and supplies a second signal having a second jitter characteristic of a second value, and wherein the second value is less than the first value; and a field carrier having an input and an output, wherein the output of the signal processing circuit is coupled to the input of the field carrier, and wherein the output of the field carrier is coupled to the second input of the signal processing circuit.
 2. The system of claim 1, wherein the field carrier is configured to carry a desired charge distribution, wherein the desired charge distribution has a first electromagnetic field, and wherein the system further comprises: a radiation source configured to generate a second electromagnetic field that interacts with the first electromagnetic field so as to produce a force on the charge carrier.
 3. The system of claim 1, wherein the first value is at least one hundred times the second value.
 4. The system of claim 1, wherein the field carrier is selected from the group consisting of: a set of wire cantilevers, and a set of traces on a printed circuit board.
 5. A signal processing circuit comprising: a first coupling circuit having a first input, a second input, a first output, and a second output, wherein the first coupling circuit is adapted to receive a first signal onto the first input, and wherein the first signal has a first jitter characteristic of a first value; and a first delay circuit having an input and an output, wherein the input of the first delay circuit is coupled to the second output of the first coupling circuit, and wherein the output of the first delay circuit is coupled to the second input of the first coupling circuit.
 6. The signal processing circuit of claim 5, wherein the first coupling circuit outputs a second signal having a second jitter characteristic of a second value, wherein the second value of the second jitter characteristic is less than the first value of the first jitter characteristic.
 7. The signal processing circuit of claim 6, wherein the first value of the first jitter characteristic is at least ten times the second value of the second jitter characteristic.
 8. The signal processing circuit of claim 5, further comprising: a second coupling circuit having a first input, a second input, and an output, wherein the first input of the second coupling circuit is coupled to the first output of the first coupling circuit; and a second delay circuit having an input and an output, wherein the output of the second delay circuit is coupled to the second input of the second coupling circuit, and wherein the output of the second coupling circuit is coupled to the input of the second delay circuit via a field carrier.
 9. The signal processing circuit of claim 8, wherein the second coupling circuit outputs a third signal having a third jitter characteristic of a third value onto the output of the second coupling circuit, wherein the third value of third jitter characteristic is less than the second value of the second jitter characteristic.
 10. The signal processing circuit of claim 9, wherein the first value of the first jitter characteristic is at least one hundred times the third value of the third jitter characteristic.
 11. The signal processing circuit of claim 8, wherein the first coupling circuit is a first broadband coupler, wherein the second coupling circuit is a second broadband coupler, wherein the first delay circuit is a first delay line, and wherein the second delay circuit is a second delay line.
 12. The signal processing circuit of claim 5, wherein the first signal has a wavelength, and wherein the first coupling circuit and the first delay circuit form a feedback loop having a length that is an integer multiple of the wavelength of the first signal.
 13. The signal processing circuit of claim 12, wherein the feedback loop operates to reduce undesirable noise present in the first signal.
 14. The signal processing circuit of claim 5, wherein the first signal is a periodic signal.
 15. A method comprising: (a) receiving a first signal onto a first feedback loop circuit, wherein the first signal has a first characteristic; (b) supplying a second signal onto a second feedback loop circuit, wherein the second signal is generated and output by the first feedback loop circuit, wherein the second signal has a second characteristic, and wherein the first characteristic is at least ten times the second characteristic; and (c) supplying a third signal onto a field carrier, wherein the third signal is generated and output by the second feedback loop circuit, wherein the third signal has a third characteristic, and wherein the second characteristic is at least ten times the third characteristic.
 16. The method of claim 15, wherein the first characteristic, the second characteristic, and the third characteristic are characterizations of signal noise.
 17. The method of claim 15, wherein the field carrier is taken from the group consisting of: a set of wire cantilevers, and a set of traces on a printed circuit board.
 18. The method of claim 15, wherein the first feedback loop circuit comprises a first coupling circuit and a first delay circuit, and wherein the second feedback loop circuit comprises a second coupling circuit and a second delay circuit.
 19. The method of claim 15, wherein each of the first signal, the second signal, and the third signal is a periodic signal that has a wavelength.
 20. The method of claim 15, wherein the first feedback loop circuit has a first feedback length that is an integer multiple of the wavelength of the first signal, and wherein the second feedback loop circuit has a second feedback length that is an integer multiple of the wavelength of the second signal. 